US1708427A - Antidetonation combustion chamber for internal-combustion engines - Google Patents
Antidetonation combustion chamber for internal-combustion engines Download PDFInfo
- Publication number
- US1708427A US1708427A US142231A US14223126A US1708427A US 1708427 A US1708427 A US 1708427A US 142231 A US142231 A US 142231A US 14223126 A US14223126 A US 14223126A US 1708427 A US1708427 A US 1708427A
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- Prior art keywords
- combustion chamber
- combustion
- antidetonation
- internal
- engine
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/22—Side valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/34—Lateral camshaft position
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- MAXMOOR CORPORATION OF NEW'YORK, N. Y., A CORPORATION OF DELAWARE.
- My invention relates to an anti-detonation combustion chamber for internal combustion engines.
- the cylinder head of an internal combustion engine in accordance with my invention has the upper wall or ceiling of the combus tion chamber therein at different heights in different parts thereof.
- the ceiling of the combustion chamber or a part thereof is formed in plural planes at varying heights above the piston.
- the language of the vertical engine is employed herein for convenience of expression, though the invention is not so limited and the cylinders may be horizontal or slanting or arranged in other ways.
- the plural planed surface of the combustion chamber is preferably confined or substantially confined to that part of the combustion chamber which is located over the cylinder bore, and in a preferred embodiment of the invention as ap- V plied to an L-head engine, the ceiling of the combustion chamber is of substantially terraced formation arranged in planes decreasing in height from near the valve side of the engine toward the further side of the cylinder bore.
- the terrace surfaces may be formed and arranged in various ways, as straight across, curved, herring-bone, and the like, and there may be a plurality of sets of terraces,
- the terraces may be arched or highest in the middle and of various other forms.
- Fig. 1 is a section of an L-head engine having a terraced combustion chamber ceiling of substantially herring-bone formation.
- Fig. 2 is a bottom plan viewof the combustion chamber of Fig. 1.
- Fig. 3 is a section on line 3-3, Fig.1.
- Fig. 4 is a section similar to Fig. 1 of an engine with a modified form of terraced formation of the combustion chamber ceiling.
- Fig. 5 is a bottom plan view of the combustion chamber of Fig. 4 having the terraces rounded out on the spark plug side.
- Fig. 6 is a section of a third form of engine.
- Fi 7 is a bottom plan view of the combustion c amber of Fig. 6, and
- Fig. 8 is a cross-section of Fig. 6.
- the portion 10 of the wall of combustion chamber- 12, which is located above the cylinder bore 14, is formed with alternate approximately vertical riser surfaces 16 and approximately plane surfaces 18, which are adapted to reduce the height of the combustion chamber in a substantial step by step fashion from the valve side of the combustion chamber toward the opposite side thereof, and the flats 18 and risers 16 are of substantially V or herringbone formation presenting the relativel pointed or angular advance portions 20 directed toward the valve side of the combustion chamber and falling back at each side of these advance portions, as indicated at 22, 22.
- the spark plug 24 is preferably located substantially opposite the prow-like or advanced portions 20.
- the substantially plane surfaces 18, 18 preferably rise to a highest elevation and substantially intersect along substantially the major axial lines of the combustion chamber and slant downwardly on each side of such axial line, substantially as shown in the sectional view, Fig. 3.
- the fiats and risers 18 and 16 instead of being of herringbone formation, are of substantially arcuate formation, and with such formation the spark plug location 28 can advantageously be moved to a position closer to one of the valves, preferably the intake valve, as shown in Fig. 5.
- the pistons 30 and 30, as shown for use in connection with the stepped combustion chamber walls of Figs. 1 and 4, are of the customary flat head construction.
- the terraced formation of the combustion chamber wall over the cylinder bore serves to produce a turbulent and agitated condition of the gases on the intake stroke, which promotes the thorough distribution of the fuel throughout the charge mixture, that upon the rising and compression of the gases against the terraced roof of the combustion chamber this thorough mixing is carried further and there is substantially a driving or forcin of the charge gases across the combustion c amber toward the valve side in a more or less wavy and lamellar manner because of the plural-plane formation of the terraced ceiling of the combustion chamber, resulting in more or less difference in the lateral movement of the gas in regions of the various strata or layers in which they are driven across the combustion chamber; and upon i ition this situation is substantially reverse the flame wave and any pressure wave occurring in connection with the flame travel being broken up and subdivided as the several riser surfacesand related plane surfaces are encountered and traversed; that there is an advantageous surface combustion effect due to gas concentrationon or adjacent to the extensive wall surface provided, and such extensive wall surface
- the rounded terraces and those of herring-bone formation are adapted to produce ad ditional cross or eddy currents and subdivisions, which serve to increase turbulence and to secure more effective breaking up of any pressure wave during the burning of the char e.
- the hlghest benefits of the present invention are realized when complete combustion and absence of carbon deposits are obtained by the use of my improved system of combustion, involving the supplying to the engine intake above the throttle of exhaust gas and air at temperatures and in proportions and quantities metered to suit the engine requirements at varying speeds and loads, as set forth, for example, in my copending application Serial No. 757,075, filed Dec. 19, 1924.
- An internal combustion engine comprising a portion of step formation in the combustion chamber thereof, and ignition means in said combustion chamber disposed laterally of and facing said portion of step formation; a part of said combustion chamber contiguous to said portion of step formation increasing in cross-sectional area towards said bustion chamber increasing in height towards the point of ignition.
- An internal combustion engine comprising a portion in the combustion chamber thereof including a plurality of horizontal surfaces disposed successively at different elevations and riser surfaces connecting the same, and ignition means disposed in said combustion chamber laterally of said portion of step formation and facing the riser sur-. faces'thereof.
- An internal combustion engine comprising a portion of step formation in the combustion chamber thereof serving to constrict the part of the combustion chamber contiguous thereto, and ignition means disposed in the larger part of said combustion chamber.
- An internal combustion engine comprising a cylinder having a combustion chamber at the end thereof extending laterally therefrom, a piston portion in said cylinder, valves in the laterally extending portion of said combustion chamber, and igniting means therein; said piston portion in the top center at the end thereof extending laterally therefrom, a piston in said cylinder, intake and exhaust valves in the laterally extending portion of said combustion chamber, and ignition means therein; apart of the ceiling of said combustion chamber over said cylinderhaving a step formation varying in height above the piston in the top center position thereof sub stantially from the valve side of the piston to the opposite side thereof, and serving to constrict the space therebetween relatively to the space occupied by said valves and said igniting means.
- a cylinder head for internal combustion engines the ceiling of the combustion chamber whereof comprises a plurality of substantially plane surfaces, which areof successively lesser height above the cylinder bore space at increasing distances from the region of ignition.
- a cylinder head for internal combustion engines the ceiling of the combustion chamber whereof over the cylinder space is of substantially terraced formation and of height increasing toward the ignition side of the combustion chamber.
- a cylinder head for internal combustion engines the height of the ceiling whereof over the piston increases by substantially well defined steps from the side furthest away from. the ignition region toward the side nearest said region.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
April 9, 1929. A. MOORE 1,708,427
ANTIDETONATION COMBUSTION CHAMBER FOR INTERNAL COMBUSTION ENGINES Filed Oct. 18. 1926 v 3 Sheets-Sheet 1 AIIIIIIMIIIIIIIIIIIJI INVENTOR ATTORNEY April 1929. A. MOORE 1,708,427
ANTIDETONATION COMBUSTION CHAMBER FOR INTERNALCOMBUSTION ENGINES Filed Oct. 18. 1926 5 Sheets-Sheet 2 INVENTOR ATTOR N EY April 1929- A. MOORE v 1,708,427
ANTIDETONATION COMBUSTION CHAMBER FOR INTERNAL COMBUSTION ENGINES Filed Oct. 18. 192 s 5 Sheets-Sheet 3 INVENTOR ATTORNEY Patented Apr. 9, 1929.
UNITED STATES ARLINGTON MOORE, OF NEW YORK, N. Y.,
PATENT OFFICE.
ASSIGNOR, BY MESNE ASSIGNMENTS, TO
MAXMOOR CORPORATION, OF NEW'YORK, N. Y., A CORPORATION OF DELAWARE.
ANTIDETONATION COMBUSTION CHAMBER FOR INTERNAL-COMBUSTION ENGINES.
Application filed October 18, 1926. Serial No. 142,231.
My invention relates to an anti-detonation combustion chamber for internal combustion engines.
The cylinder head of an internal combustion engine in accordance with my invention has the upper wall or ceiling of the combus tion chamber therein at different heights in different parts thereof. Preferably the ceiling of the combustion chamber or a part thereof is formed in plural planes at varying heights above the piston. The language of the vertical engine is employed herein for convenience of expression, though the invention is not so limited and the cylinders may be horizontal or slanting or arranged in other ways.
In the case of a side valve engine, and particularly an L-head engine, the plural planed surface of the combustion chamber is preferably confined or substantially confined to that part of the combustion chamber which is located over the cylinder bore, and in a preferred embodiment of the invention as ap- V plied to an L-head engine, the ceiling of the combustion chamber is of substantially terraced formation arranged in planes decreasing in height from near the valve side of the engine toward the further side of the cylinder bore. The terrace surfaces may be formed and arranged in various ways, as straight across, curved, herring-bone, and the like, and there may be a plurality of sets of terraces,
' the terraces may be arched or highest in the middle and of various other forms.
My invention will be best understood from a description of the illustrative embodiments shown in the accompanying drawings, in which Fig. 1 is a section of an L-head engine having a terraced combustion chamber ceiling of substantially herring-bone formation. Fig. 2 is a bottom plan viewof the combustion chamber of Fig. 1. Fig. 3 is a section on line 3-3, Fig.1. Fig. 4 is a section similar to Fig. 1 of an engine with a modified form of terraced formation of the combustion chamber ceiling. Fig. 5 is a bottom plan view of the combustion chamber of Fig. 4 having the terraces rounded out on the spark plug side. Fig. 6 is a section of a third form of engine. Fi 7 is a bottom plan view of the combustion c amber of Fig. 6, and Fig. 8 is a cross-section of Fig. 6.
In the form shown in Figs. 1, 2 and 3,the portion 10 of the wall of combustion chamber- 12, which is located above the cylinder bore 14, is formed with alternate approximately vertical riser surfaces 16 and approximately plane surfaces 18, which are adapted to reduce the height of the combustion chamber in a substantial step by step fashion from the valve side of the combustion chamber toward the opposite side thereof, and the flats 18 and risers 16 are of substantially V or herringbone formation presenting the relativel pointed or angular advance portions 20 directed toward the valve side of the combustion chamber and falling back at each side of these advance portions, as indicated at 22, 22. The spark plug 24 is preferably located substantially opposite the prow-like or advanced portions 20. The substantially plane surfaces 18, 18 preferably rise to a highest elevation and substantially intersect along substantially the major axial lines of the combustion chamber and slant downwardly on each side of such axial line, substantially as shown in the sectional view, Fig. 3.
In the form of Figs. 4; and 5 the fiats and risers 18 and 16 instead of being of herringbone formation, are of substantially arcuate formation, and with such formation the spark plug location 28 can advantageously be moved to a position closer to one of the valves, preferably the intake valve, as shown in Fig. 5. The pistons 30 and 30, as shown for use in connection with the stepped combustion chamber walls of Figs. 1 and 4, are of the customary flat head construction.
In the form of Figs. 6, 7 and 8 the flats and risers 18 and 16 run substantially straight across the combustion chamber wall at right angles to the major axis thereof and, with this arrangement, the spark plug location 28 is substantially opposite the middle of the stepped surfaces so provided.
Without commitment to a particular theory, it is my belief that the terraced formation of the combustion chamber wall over the cylinder bore serves to produce a turbulent and agitated condition of the gases on the intake stroke, which promotes the thorough distribution of the fuel throughout the charge mixture, that upon the rising and compression of the gases against the terraced roof of the combustion chamber this thorough mixing is carried further and there is substantially a driving or forcin of the charge gases across the combustion c amber toward the valve side in a more or less wavy and lamellar manner because of the plural-plane formation of the terraced ceiling of the combustion chamber, resulting in more or less difference in the lateral movement of the gas in regions of the various strata or layers in which they are driven across the combustion chamber; and upon i ition this situation is substantially reverse the flame wave and any pressure wave occurring in connection with the flame travel being broken up and subdivided as the several riser surfacesand related plane surfaces are encountered and traversed; that there is an advantageous surface combustion effect due to gas concentrationon or adjacent to the extensive wall surface provided, and such extensive wall surface ermits reduction of combustion chamber c earance volume without reduction in surface area, and even with actual increase thereof, and the resulting. effective delivery of heat to the water jacket will avoid excessive rise of temperature, which' would produce detonation and, by acting to withdraw heat which is carried away from regions of incipient incandescence by the highly turbu lent movement of the charge gases, will prevent preignition. The rounded terraces and those of herring-bone formation, in addition to the foregoing, are adapted to produce ad ditional cross or eddy currents and subdivisions, which serve to increase turbulence and to secure more effective breaking up of any pressure wave during the burning of the char e.
The hlghest benefits of the present invention are realized when complete combustion and absence of carbon deposits are obtained by the use of my improved system of combustion, involving the supplying to the engine intake above the throttle of exhaust gas and air at temperatures and in proportions and quantities metered to suit the engine requirements at varying speeds and loads, as set forth, for example, in my copending application Serial No. 757,075, filed Dec. 19, 1924.
I claim:
1. An internal combustion engine comprising a portion of step formation in the combustion chamber thereof, and ignition means in said combustion chamber disposed laterally of and facing said portion of step formation; a part of said combustion chamber contiguous to said portion of step formation increasing in cross-sectional area towards said bustion chamber increasing in height towards the point of ignition.
4. An internal combustion engine comprising a portion in the combustion chamber thereof including a plurality of horizontal surfaces disposed successively at different elevations and riser surfaces connecting the same, and ignition means disposed in said combustion chamber laterally of said portion of step formation and facing the riser sur-. faces'thereof.
5. An internal combustion engine comprising a portion of step formation in the combustion chamber thereof serving to constrict the part of the combustion chamber contiguous thereto, and ignition means disposed in the larger part of said combustion chamber.
6. An internal combustion engine comprising a cylinder having a combustion chamber at the end thereof extending laterally therefrom, a piston portion in said cylinder, valves in the laterally extending portion of said combustion chamber, and igniting means therein; said piston portion in the top center at the end thereof extending laterally therefrom, a piston in said cylinder, intake and exhaust valves in the laterally extending portion of said combustion chamber, and ignition means therein; apart of the ceiling of said combustion chamber over said cylinderhaving a step formation varying in height above the piston in the top center position thereof sub stantially from the valve side of the piston to the opposite side thereof, and serving to constrict the space therebetween relatively to the space occupied by said valves and said igniting means.
8. A cylinder head for internal combustion engines, the ceiling of the combustion chamber whereof comprises a plurality of substantially plane surfaces, which areof successively lesser height above the cylinder bore space at increasing distances from the region of ignition.
9. A cylinder head for internal combustion engines, the ceiling of the combustion chamber whereof over the cylinder space is of substantially terraced formation and of height increasing toward the ignition side of the combustion chamber.
'10. A cylinder head for internal combustion engines, the height of the ceiling whereof over the piston increases by substantially well defined steps from the side furthest away from. the ignition region toward the side nearest said region.
11. In an internal combustion engine commation decreasing in height above the piston substantially from the valve side of the piston to the op site side thereof In testlmony whereof, I have signed my name hereto:
ARLING-TGN oosnn
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US142231A US1708427A (en) | 1926-10-18 | 1926-10-18 | Antidetonation combustion chamber for internal-combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US142231A US1708427A (en) | 1926-10-18 | 1926-10-18 | Antidetonation combustion chamber for internal-combustion engines |
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US1708427A true US1708427A (en) | 1929-04-09 |
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US142231A Expired - Lifetime US1708427A (en) | 1926-10-18 | 1926-10-18 | Antidetonation combustion chamber for internal-combustion engines |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4467752A (en) * | 1982-06-21 | 1984-08-28 | Motortech, Inc. | Internal combustion engine |
-
1926
- 1926-10-18 US US142231A patent/US1708427A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4467752A (en) * | 1982-06-21 | 1984-08-28 | Motortech, Inc. | Internal combustion engine |
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